US7459215B2 - Carbon fiber composite transfer member with reflective surfaces - Google Patents
Carbon fiber composite transfer member with reflective surfaces Download PDFInfo
- Publication number
- US7459215B2 US7459215B2 US10/519,029 US51902904A US7459215B2 US 7459215 B2 US7459215 B2 US 7459215B2 US 51902904 A US51902904 A US 51902904A US 7459215 B2 US7459215 B2 US 7459215B2
- Authority
- US
- United States
- Prior art keywords
- carbon
- transfer member
- reinforced composite
- fiber
- composite material
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related, expires
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Images
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- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/20—Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
- B32B2307/21—Anti-static
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/40—Properties of the layers or laminate having particular optical properties
- B32B2307/416—Reflective
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/56—Damping, energy absorption
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/02—Noble metals
- B32B2311/04—Gold
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/02—Noble metals
- B32B2311/08—Silver
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/12—Copper
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/16—Tin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/18—Titanium
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/22—Nickel or cobalt
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/24—Aluminium
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/30—Iron, e.g. steel
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2457/00—Electrical equipment
- B32B2457/20—Displays, e.g. liquid crystal displays, plasma displays
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L21/00—Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
- H01L21/67—Apparatus specially adapted for handling semiconductor or electric solid state devices during manufacture or treatment thereof; Apparatus specially adapted for handling wafers during manufacture or treatment of semiconductor or electric solid state devices or components ; Apparatus not specifically provided for elsewhere
- H01L21/677—Apparatus specially adapted for handling semiconductor or electric solid state devices during manufacture or treatment thereof; Apparatus specially adapted for handling wafers during manufacture or treatment of semiconductor or electric solid state devices or components ; Apparatus not specifically provided for elsewhere for conveying, e.g. between different workstations
- H01L21/67739—Apparatus specially adapted for handling semiconductor or electric solid state devices during manufacture or treatment thereof; Apparatus specially adapted for handling wafers during manufacture or treatment of semiconductor or electric solid state devices or components ; Apparatus not specifically provided for elsewhere for conveying, e.g. between different workstations into and out of processing chamber
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31511—Of epoxy ether
- Y10T428/31529—Next to metal
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31678—Of metal
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/20—Control lever and linkage systems
- Y10T74/20207—Multiple controlling elements for single controlled element
- Y10T74/20305—Robotic arm
Definitions
- the present invention relates to a transfer member. More particularly, the present invention relates to a carbon fiber composite transfer member with reflective surfaces that is suitable for transferring flat panel displays without energy absorption.
- the beta titanium-composite laminate comprises a first layer of beta titanium alloy having a certain yield strength to modulus of elasticity ratio and adhering a first layer of composite having a certain strength to modulus of elasticity ratio to the layer of beta titanium alloy, thereby forming a beta titanium-composite laminate, where the yield strength to modulus of elasticity ratio of the first layer of beta titanium alloy matches the strength to modulus of elasticity ratio of the first layer of composite such that the first layer of beta titanium alloy will reach its stress limit and the first layer of composite will reach its stress limits at about the same total strain.
- the hybrid laminates include lay-ups of layers of titanium alloy foil and composite plies, that are optimally oriented to counteract forces encountered in use and are bonded to a central core structure, such as titanium alloy honeycomb.
- the reinforcing fibers of the composite plies are selected from carbon and boron, and the fibers are continuous and parallel oriented within each ply. However, some plies may be oriented at angles to other plies. Nevertheless, in a preferred embodiment of the invention, a substantial majority of, or all of, the fibers of the hybrid laminates are oriented in a common direction.
- the outer surfaces of the laminates include a layer of titanium foil to protect the underlying composite-containing structure from the environment, and attack by solvents, and the like.
- U.S. Pat. No. 4,888,247 to Zweben et al. discloses heat conducting laminates and laminated heat conducting devices, having at least one layer of metal and at least one layer of polymer matrix composite material having low-thermal-expansion reinforcing material distributed throughout and embedded therein.
- the coefficient of thermal expansion and the thermal conductivity of the laminated heat conducting devices are defined by the metal in combination with the polymer matrix material and low-thermal-expansion reinforcing material in the laminate.
- the coefficient of thermal expansion and thermal conductivity of a heat conducting device can be controlled by bonding at least one layer of metal to at least one layer of polymer matrix composite material having low-thermal-expansion reinforcing material distributed throughout and embedded therein.
- the laminated heat conducting device comprises a plurality of alternating layers of aluminum and epoxy resin having graphite fibers distributed throughout the epoxy resin.
- U.S. Pat. No. 3,939,024 to Hoggatt discloses structural reinforced thermoplastic laminates capable of supporting loads in at least two directions and containing by volume about 45% to 65% fiber reinforcement.
- the laminates can be used with or without metal cladding.
- a transfer member for transferring these components is used.
- a transfer member may be installed in a device such as an industrial robot for moving precision devices. The components are placed or held on the transfer member and moved to the desired location.
- high temperature displays are transferred between process steps by automatic robotics. These robots have end effectors (e.g. support arms) that lift and provide a resting place for the display panels during their transport. Ceramic and aluminum have historically been used as the end effector material due to their stiffness and purity levels. Recently, CFRP (carbon fiber reinforced plastic) has been introduced as end effectors because of their stiffness, cost and vibration damping properties have been desirable.
- CFRP carbon fiber reinforced plastic
- CFRPs are black in color and absorb radiant thermal energy from the display panel during transport which is detrimental to flat panel displays because too much heat transfer can damage the flat panel display or other heat sensitive material. This feature limits the market of CFRP end effectors in flat panel display manufacturing were it is important not to absorb radiant thermal energy.
- a transfer member e.g. support arms or end effectors
- CFRP flat panel display transport
- a transporting member comprising:
- FIG. 1 shows a top view of an end effector or support arm used for transport in the present invention
- FIG. 2 shows cross-sectional view of the layers of the transfer member in the present invention
- FIG. 3 shows a top view showing another example of the transfer member
- FIG. 4 shows a cross-sectional view of the transfer member (i.e. end effector, support arm, body) is cut by a vertical section, including its longitudinal direction.
- the transfer member i.e. end effector, support arm, body
- the present invention is a transfer member that provides a reflective surface that prevents energy absorption by the carbon fiber-reinforced plastic used in end effectors or support arms to transport precision devices that include flat panel displays and semi-conductors.
- precision devices such as flat panel displays and semi-conductors are transferred between process steps by automatic robotics.
- the carbon-fiber-reinforced composite material of the transfer member body includes at least one layer of a unidirectional prepreg in which carbon fibers are arranged essentially parallel with the longitudinal direction of the body.
- the carbon-fiber-reinforced composite material of the body includes at least one layer of a cloth prepreg containing carbon fibers, with at least part of the carbon fibers of the prepreg and the electroconductive polymer part being electrically connected.
- each layer of the composite body preferably ranges from about 0.02 mm to about 1.00 mm in thickness.
- the carbon-fiber-reinforced composite material of the transfer member includes: a carbon-fiber-reinforced plastic (CFRP) and a carbon-fiber-reinforced carbon composite material (C/C composite material).
- CFRP carbon-fiber-reinforced plastic
- the CFRP material is preferred.
- the matrix material of the carbon-fiber-reinforced composite material comprises: a thermosetting polymer, a thermoplastic polymer, carbon, ceramic, metal, and mixtures thereof. In the present invention, a thermosetting polymer, carbon, or a mixture thereof is preferable as the matrix.
- thermosetting polymer includes: an epoxy, aramid, bismaleimide, phenol, furan, urea, unsaturated polyester, epoxy acrylate, diallyl phthalate, vinyl ester, thermosetting polyimide, melamine, and other such materials.
- the thermoplastic polymer matrix material for the present invention includes: polyimide resin, nylon, liquid aromatic polyamide, polyester, liquid aromatic polyester, polypropylene, polyether sulfone polymer, polyphenylene sulfide, PEEK (polyether ether ketone), PEK (polyetherketone) PEKK (polyether ketone), LCP (liquid crystal polymer), polysulfone, polyvinyl chloride, vinylon, aramid, fluoropolymer, and other such materials.
- the ceramic matrix material for the present invention includes: alumina, silica, titanium carbide, silicon carbide, boron nitride, silicon nitride, and other such materials.
- Metal matrix materials for the present invention include: titanium, aluminum, tin, silicon, copper, iron, magnesium, chromium, nickel, molybdenum, tungsten, and alloys containing one or more of these metals.
- the carbon fibers included in the above-mentioned carbon-fiber-reinforced composite material comprise: petroleum pitch-type carbon fibers, coal pitch-type carbon fibers, polyacrylonitride (PAN) carbon fibers, and other such fibers.
- the electric resistivity of the carbon fibers is normally from 1-30 ⁇ m, and preferably 1-20 ⁇ m.
- the carbon-fiber-reinforced composite material may include only one kind of carbon fibers and can also include a hybrid structure of two or more kinds of these carbon fibers.
- the form of the carbon fibers used in the carbon-fiber-reinforced composite material include one-dimensional reinforcing, two-dimensional reinforcing, three-dimensional reinforcing, random reinforcing, and similar forms are appropriately selected and adopted in accordance with the desired purpose of the transfer member.
- the carbon fibers may be in the form of short fibers, woven fabric, nonwoven fabric, unidirectional material, two-dimensional woven fabric, and three-dimensional woven fabric as desired. More specifically, the carbon fibers may be used in a material with the structure of felt, mat, braided fabric (i.e.
- nonwoven fabric comprising carbon fibers arranged in parallel crosses or triangular form with hot-melt polymer), unidirectional material, pseudo-isotropic material, plain fabric, satin, twilled fabric, pseudo thin fabric, entangled fabric, etc., laminated and then can be installed in the above-mentioned carbon-fiber-reinforced composite material.
- the electroconductive polymer part is electrically connected to at least part of the carbon fibers in the body.
- the body makes contact with the article when the article is transferred.
- a portion of the electroconductive polymer part is in contact with the transferred article placed thereon.
- the contact, between the article and the body, is electrically connected to the electroconductive polymer part via the carbon fibers.
- the present invention further provides contact to a grounding conductor.
- the electroconductive polymer part includes a polyimide polymer.
- the polymer material has electrical conductivity.
- a polymer material in which an electroconductive filler is added to a thermosetting or thermoplastic polymer include: a fluoropolymer, PAI (polyamideimide), PA (polyamide), PEI (polyetherimide), POM (polyoxymethylene), PEEK (polyetheretherketone, PEKK (polyetherketoneketone), PEK (polyetherketone), polyacetate, nylon polymer, aromatic polyimide, polyethersulfon (PES), polyimide, polyetherimide, polyester, liquid crystal polymer (LCP), polybenzimidazole (PBI), Poly(paraphenylene benzobisaxazole) (PBO), polyphenylene sulfide (PPS), polycarbonate (PC), polyacrylate, polyacetal, or mixture of two or more thereof.
- PAI polyamideimide
- PA polyamide
- PEI polyetherimide
- electroconductive fillers for use in the present invention include: metal powders, carbon black, carbon fibers, zinc oxide titanium oxide, potassium titanate. It is preferable, that the polymer material contain a polyimide that has excellent abrasive resistance, antistatic property and chemical resistance; has dimensional stability and mechanical processability for manufacturing a transfer member; and does not easily damage articles such as glass substrates or wafers when making contact with them; and does not easily generate particles.
- the volume resistivity of the electroconductive polymer part normally ranges from 10 1 -10 12 ⁇ cm, and preferably from 10 4 -10 5 ⁇ cm.
- a manufacturing method for making the transfer member may include preparing a transfer member body containing a carbon-fiber-reinforced composite material. The process exposes a portion of the carbon fibers of the composite material, and an electroconductive polymer part is installed on the transfer member body such that it can be electrically connected to the exposed carbon fibers. The electroconductive polymer part is installed by bonding the transfer member body and the electroconductive polymer part with an electroconductive adhesive.
- the manufacturing method for installation of the electroconductive polymer part comprises inserting the electroconductive polymer part into a hole or concave part.
- the hole and concave part are formed in a way to expose the internal carbon fibers of the composite material.
- Another aspect of the present invention is the method of manufacturing a transfer member with electric conductivity.
- a method for manufacturing the carbon-fiber-reinforced composite material such as CFRP and C/C composite material known in the art can be used.
- the CFRP can be prepared by forming a prepreg by impregnating reinforcing carbon fibers with a thermosetting polymer, then laminating and curing them.
- the CFRP with a prescribed elastic modulus by laminating the prepreg of unidirectional reinforcing carbon fibers, that is, unidirectional prepreg so that the direction of the fibers is 0° and 90°, 0°, ⁇ 45°, and 90° or 0°, ⁇ 60°, and 90° with respect to the longitudinal direction of the transfer part.
- thermosetting polymer In the impregnation of the reinforcing carbon fibers into the thermosetting polymer, a hot-melt method, that usually heats the polymer to 60-90° C. and impregnates it on the reinforcing fibers, is preferably applied.
- the content of the thermosetting polymer in the prepreg manufacture is usually 20-50 wt %, and preferably 25-45 wt %, relative to the total weight of the reinforcing fibers.
- a filler can be added to the polymer constituting the prepreg.
- the filler material includes: mica, alumina, talc, fine powder-shaped silica, wollastonite, sepiolite, basic magnesium sulfate, calcium carbonate, polytetrafluoroethylene powder, zinc powder, aluminum powder, and organic fine particles such as fine acryl particles, fine epoxy polymer particles, fine polyamide particles, and fine polyurethane particles and other such materials or a combination of two or more of any of the above.
- the prepreg is laminated in an appropriate shape on the transfer part and heated and cured at 110-150° C. for 30 min-3 hr in an autoclave or by a press, so that the CFRP can be obtained. With such a method, CFRP with stable qualities and little voids can be obtained.
- the C/C composite material can also be manufactured by a known method.
- carbon fibers are used in a form similar to the carbon fibers used for the CFRP manufacture described above.
- a preform i.e. a shape formed at an intermediate step of the process
- a matrix polymer such as a thermoplastic polymer and thermosetting polymer
- Carbonization can be carried out by heating the preform as described above at 500° C., preferably, 300° C., in an inert gas.
- the C/C composite includes a pitch substance such as those using coal pitch, petroleum pitch, synthetic pitch, isotropic pitch, and meso-phase pitch as raw materials.
- a thermoplastic polymer that may include: polyimide resin, phenol polymer, epoxy polymer, furan polymer and urea polymer and a thermosetting polymer comprises phenol polymer, epoxy polymer, furan polymer, urea polymer and other such materials.
- the pitch, thermosetting polymer, or thermoplastic polymer can also be mixed with a filler and provided to the process for forming the matrix.
- filler material include: carbon powders, graphite powders, silicon carbide powders, silica powders, carbon fiber whiskers, carbon short fibers, and silicon carbon short fibers.
- Another example of the method for manufacturing the C/C composite material is forming a matrix by attaching a thermally decomposable carbon to carbon fibers using chemical vapor deposition (CVD), chemical vapor infiltration (CVI), or such similar process creating the C/C composite material can be prepared.
- CVD chemical vapor deposition
- CVI chemical vapor infiltration
- the C/C composite material obtained in this manner can be further subjected to a miniaturization treatment.
- the density of the composite material can be improved by repeating the matrix forming process.
- the body of the transfer member of the present invention may be formed from just the carbon-fiber-reinforced composite material or, from the combination of the carbon-fiber-reinforced composite fiber and other materials such as a glass fiber reinforced plastic (GFRP).
- the other materials include structures such as a honeycomb, a porous body, or a corrugated plate.
- the body can be prepared by subjecting the molded body, containing the carbon-fiber-reinforced composite material obtained using the method described above, to a process such as cutting the body to the desired shape. With such processing, the body having the desired form can be obtained with accurate working precision. Furthermore, an electrical connection of the carbon fibers and the electroconductive polymer part can be easily achieved as will be described subsequently. And, if necessary, the body can have coating agents applied to prevent particle generation from the working surface. A thermosetting polymer such as an epoxy polymer and silicone wax can be used as the coating agent.
- An example of the transfer member body of the present invention is an oblong plate-shaped structure with skin layers positioned on both surfaces of the plate and a core layer positioned between the skin layers. The top and bottom surfaces of the structure are covered with an epoxy coated, metal film forming a reflective surface.
- each skin layer of the transfer member body preferably ranges from about 0.02 mm to about 1.00 mm in thickness.
- the skin layers have a first carbon-fiber-reinforced composite material layer containing carbon fibers, that are oriented at an angle of ⁇ 20° to +20° with respect to the longitudinal direction of the transfer part and have a tensile elastic modulus of 500-1,000 GPa.
- the second layer is a carbon-fiber-reinforced composite material layer containing carbon fibers, that are oriented at an angle of +75° to +90° and/or ⁇ 75° to ⁇ 90° with respect to the longitudinal direction of the transfer part and have a tensile elastic modulus of 200-400 GPa.
- the skin layers have a third carbon-fiber reinforced composite fiber that is oriented at an angle of +30° to +60° and/or ⁇ 30° to ⁇ 60° with respect to the longitudinal direction of the transfer part and has a tensile elastic modulus of 500-1,000 GPa.
- the ratio of the thickness of the three skin layers to the total thickness of the skin layers and the core layer is 20-80%, preferably 60-80%.
- the contact can be electrically connected to the polymer electroconductive part via carbon fibers of the skin layers.
- the core layer in addition to or instead of, the above-mentioned third skin layer of carbon-fiber-reinforced composite material, may include another material layer with a structure such as a honeycomb, porous body, and/or a waved plate (corrugated) and voids may also be used.
- a cloth layer made of fibrous materials such as carbon fibers can be disposed on the outermost surface of the body making it easier to process the transfer members than if the cloth layer was not present. And, if the cloth layers are made of carbon fiber, the electronic connection between the contact and electroconductive polymer part becomes easier.
- An embodiment of the transfer member of the present invention includes a body having a carbon-fiber-reinforced composite material and an electroconductive polymer part being electrically connected to at least part of the carbon fibers in the body and having a portion for contact with a transferred article by placing it on the body.
- the area where the transfer member makes contact with the article may be the surface of the distal end of the transfer member, and the electroconductive polymer part.
- the electrical connection of the electroconductive polymer part with at least part of the carbon fibers of the body can be achieved by: exposing a portion of the carbon fibers of the carbon-fiber-reinforced composite material contained in the body, and installing the electroconductive polymer part on the body so that it can be electrically connected with the carbon fibers exposed.
- the carbon fibers may be exposed by forming the transfer member body as a molded body containing the carbon-fiber-reinforced composite material and forming a hole or concave part by cutting a portion thereof. (e.g. Normally, when a molded body containing a carbon-fiber-reinforced composite material is manufactured, its surface is coated with a matrix, and the carbon fibers are not exposed.
- the glass fiber epoxy resin layer comprises a combination of glass fiber material and epoxy resin material.
- the glass fiber material includes S-glass, E-glass, and D-glass and examples of epoxy resin materials include condensation products of epichlorohydrin and bisphenol-A.
- the electrical connection of the exposed carbon fibers and the electroconductive polymer part may occur by bonding the body and the electroconductive polymer part with an electroconductive adhesive at a different portion of the electroconductive polymer part then the portion for contact with a transferred article on the surface of the body containing the cut surface or by inserting the electroconductive polymer part into the hole or concave part formed in the process for exposing the carbon fibers of the body.
- a method for bonding the body and the electroconductive polymer part is not critical, any method in which the electroconductive polymer part can be electrically connected with at least part of the carbon fiber forming the body and another portion where a transferred article may be placed in contact therewith may be used.
- the transfer part of the present invention may be equipped with only one electroconductive polymer part or with several electroconductive polymer parts. When several electroconductive polymer parts are used, one or more of them can be electrically connected to the carbon fibers.
- the transfer part of the present invention can be further equipped with a contact to a grounding conductor.
- the above-mentioned contact is electrically connected with the electroconductive polymer part via at least part of the carbon fibers, so that the static electricity of an article making contact with the electroconductive polymer part can be removed by the grounding method.
- the above-mentioned contact may be simply that of the exposed surface of the carbon fibers formed by cutting of the body or it may also be a desired metal electrode.
- the shape of the transfer part of the present invention can be oblong as mentioned above, however, a variety of shapes including a plate shape, rod shape, fork shape, honeycomb shape, hollow rod shape, T shape, I shape, curved surface shape, or a combined shape can also be adopted for use in the present invention.
- the transfer member of the present invention can have an area in contact with the transferred article at its distal end or can have the contact at its proximal end.
- the transfer member of the present invention may have a shape in which only the electroconductive polymer part makes contact with the transferred article and supports it or, a shape in which both the electroconductive polymer part and the body make contact with the transferred article and support it.
- the proximal end is fixed to a device for moving the transfer member such as an industrial robot. The device is operated such that the article being transferred may be placed or held at the distal end to enable transfer of the article.
- FIG. 1 shows a topical view of an embodiment of the present invention where an end effector or support arm or body 10 has a fork-shaped structure.
- the body 10 has a portion 20 of the transfer member that holds the article (e.g. precision device) being transferred.
- the handle portion 25 is attached to the article holding portion 20 .
- the body 10 is formed from a core material such as a carbon fiber composite material and then additional layers as described in FIG. 2 .
- part or all of the carbon fibers are arranged essentially parallel with the longitudinal direction, that is, the distal position-proximal position direction of the body 10 .
- An electroconductive polymer part 22 is mounted at a position shown in FIG. 1 , so that it is electrically connected to a contact 26 via the carbon fibers.
- the grounding conductor 24 is connected to the contact 26 in removing the current (i.e discharging the static electricity).
- the body of the present invention is made up of layers shown in the cross-sectional view of a portion of the body.
- the body 10 (see FIG. 1 ) is composed of layers that include: a carbon fiber composite layer 50 that has a top surface 51 and a bottom surface 52 .
- a metal film 61 , 62 is applied to the top surface 51 and the bottom surface 52 , respectively, of the carbon-fiber reinforced plastic material 50 .
- the metal film 61 , 62 includes at least one of the following: titanium, copper, aluminum, steel, gold, silver, nickel, tin, and/or combinations thereof.
- This metal film 61 , 62 provides the reflective surface that prevents energy absorption by the CFRP during transport in the present invention. This is particularly useful for the transport of precision devices such as flat panel displays and other such devices in which energy absorption by the transport material can occur.
- This metal film 61 , 62 is preferably titanium.
- a glass fiber epoxy resin layer 71 , 72 is applied to the metal film 61 (top surface layer) and 62 (bottom surface layer), respectively.
- the glass fiber expoxy resin layers 71 , 72 are applied to opposite sides of the metal film 61 and 62 than those sides in contact with the carbon-fiber reinforced plastic material 50 .
- the translucent layer of the glass fiber and epoxy layer provide see through and protective fiber for the metal film.
- the composite layers shown in FIG. 2 of the present invention will not absorb thermal energy and can be utilized as end effectors in the transport of temperature sensitive flat panel displays.
- the carbon-fiber-reinforced composite layer of the body includes a non purity of less than 30 ppm, preferably less than 15 ppm water and less than 5 ppm, preferably less than 1 ppm hydrogen gas being evolved at a vacuum of 10-5 Pa, having a temperature condition of from 25° C. to 250° C. at a ramp up rate of 10° C./minute.
- FIG. 3 shows a top view of another embodiment of the transfer member of the present invention.
- a body 31 has a fork-shaped structure, and an electroconductive polymer part 32 is mounted in each of its branched ends.
- the body 31 is formed by laminating cloth prepreg sheets.
- carbon fibers in the cloth prepregs are crossed and extended in the longitudinal direction and the width direction of the transfer member body 31 . Therefore, the electroconductive polymer part 32 is electrically connected to a contact 36 via said carbon fibers, and in transferring an article, the article makes contact with the electroconductive polymer part 32 , so that a current flows in the arrow direction 33 , thereby removing the current (i.e. discharging the static electricity).
- the grounding conductor 34 is connected to the contact 36 in a similar manner as described in FIG. 1 .
- FIG. 4 is a cross section in which the transfer member is cut by a vertical section, including its longitudinal direction.
- the body 11 has an oblong plate shape, and is formed of a carbon-fiber-reinforced composite material, and has a concave part 15 on the upper surface of its distal end.
- the concave part 15 is produced by forming a molded body composed of a carbon-fiber-reinforced composite material and cuffing it in the shape shown.
- An electroconductive polymer part 12 has a convex part fitting into the concave part 15 and is mounted in the body 11 via an electroconductive adhesive or by press-fitting it into the concave part 15 .
- a contact 16 to a grounding conductor 14 is installed and connected to the grounding conductor 14 .
- the contact 16 may be directly connected to the grounding conductor 14 or may also be grounded via a device such as an industrial robot for moving the transfer member.
- the contact 16 can also have a structure fitted to each ground shape.
- the body 11 is formed by laminating unidirectional prepreg sheets. In the body 11 , part or all of the carbon fibers of composite layer 50 are arranged substantially parallel with the longitudinal direction of the body 11 , that is, in the distal position to proximal position direction.
- the electroconductive polymer part 12 and the contact 16 are electrically connected via the carbon fibers of the body 11 , and in transferring an article, the article makes contact with the electroconductive polymer part 12 , so that a current flows in the arrow 13 direction, thereby removing the current.
- the transfer member of the present invention comprises a body comprising a carbon-fiber-reinforced composite material and an electroconductive polymer part being electrically connected to at least part of the carbon fibers in said body and having a portion for contact with a transferred article by it being placed on, can improve transferability of a transferred article such as silicon wafer for semiconductor and liquid crystal glass substrate by a transfer member, suppress damage to the transferred articles caused by a transferring environment and be easily manufactured, and has lightness, high stiffness, and high heat resistance due to the body containing a fiber reinforced composite material and the electroconductive polymer part associated with the body, in addition, can effectively remove the static electricity of an article by the grounding method.
- the transfer part is very useful in a similar manner as described in FIG. 1 .
- the article makes contact with the electroconductive polymer part 32 , so that a current flows in the arrow direction 33 .
- the above-mentioned transfer part can be manufactured in a simple manner.
Landscapes
- Engineering & Computer Science (AREA)
- Robotics (AREA)
- Mechanical Engineering (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- General Physics & Mathematics (AREA)
- Manufacturing & Machinery (AREA)
- Computer Hardware Design (AREA)
- Physics & Mathematics (AREA)
- Power Engineering (AREA)
- Ceramic Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Laminated Bodies (AREA)
- Inorganic Fibers (AREA)
- Carbon And Carbon Compounds (AREA)
- Chemical Or Physical Treatment Of Fibers (AREA)
Abstract
Description
- a) a body having a carbon-fiber reinforced composite material, said body having a top surface and a bottom surface;
- b) a metal film covering the top and bottom surfaces of the composite body, said film forming a reflective surface; and
- c) a glass fiber epoxy resin forming a layer on the metal film covering the top surface and the bottom surface of the body.
Claims (2)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/519,029 US7459215B2 (en) | 2002-07-29 | 2002-12-02 | Carbon fiber composite transfer member with reflective surfaces |
US12/259,816 US7871705B2 (en) | 2002-07-29 | 2008-10-28 | Carbon fiber composite transfer member with reflective surfaces |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US39933702P | 2002-07-29 | 2002-07-29 | |
PCT/US2002/041652 WO2004011248A1 (en) | 2002-07-29 | 2002-12-02 | Carbon fiber composite transfer member with reflective surfaces |
US10/519,029 US7459215B2 (en) | 2002-07-29 | 2002-12-02 | Carbon fiber composite transfer member with reflective surfaces |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US12/259,816 Division US7871705B2 (en) | 2002-07-29 | 2008-10-28 | Carbon fiber composite transfer member with reflective surfaces |
Publications (2)
Publication Number | Publication Date |
---|---|
US20060153669A1 US20060153669A1 (en) | 2006-07-13 |
US7459215B2 true US7459215B2 (en) | 2008-12-02 |
Family
ID=31188571
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/519,029 Expired - Fee Related US7459215B2 (en) | 2002-07-29 | 2002-12-02 | Carbon fiber composite transfer member with reflective surfaces |
US12/259,816 Expired - Fee Related US7871705B2 (en) | 2002-07-29 | 2008-10-28 | Carbon fiber composite transfer member with reflective surfaces |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US12/259,816 Expired - Fee Related US7871705B2 (en) | 2002-07-29 | 2008-10-28 | Carbon fiber composite transfer member with reflective surfaces |
Country Status (13)
Country | Link |
---|---|
US (2) | US7459215B2 (en) |
EP (1) | EP1525088B1 (en) |
JP (1) | JP4474601B2 (en) |
KR (1) | KR100989012B1 (en) |
CN (1) | CN100415505C (en) |
AT (1) | ATE500057T1 (en) |
AU (1) | AU2002361894A1 (en) |
CA (1) | CA2493963C (en) |
DE (1) | DE60239361D1 (en) |
ES (1) | ES2361827T3 (en) |
IL (1) | IL165937A0 (en) |
TW (1) | TW200401704A (en) |
WO (1) | WO2004011248A1 (en) |
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US9388278B2 (en) | 2013-10-04 | 2016-07-12 | Industrial Technology Research Institute | Release layer, substrate structure, and method for manufacturing flexible electronic device |
US9884426B2 (en) | 2013-06-27 | 2018-02-06 | De-Sta-Co Europe Gmbh | Boom utilized in a geometric end effector system |
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TWI701213B (en) * | 2018-05-21 | 2020-08-11 | 態金材料科技股份有限公司 | Carbon fiber core material surface is welded with alloy film layer to make composite material and its products. |
KR20220081216A (en) * | 2020-12-08 | 2022-06-15 | 주식회사 글린트머티리얼즈 | Heat resistant and conductive anti-slip pad for transfering semiconductor wafer |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4759964A (en) * | 1983-10-10 | 1988-07-26 | Fischer Gesellschaft M.B.H. | Structural panel |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1562569A (en) * | 1975-12-04 | 1980-03-12 | United Glass Ltd | Materials for handling hot glassware and other hot articles |
US4888247A (en) * | 1986-08-27 | 1989-12-19 | General Electric Company | Low-thermal-expansion, heat conducting laminates having layers of metal and reinforced polymer matrix composite |
US4961994A (en) * | 1987-12-16 | 1990-10-09 | General Electric Company | Protective coated composite material |
JPH01277665A (en) * | 1988-04-30 | 1989-11-08 | Toyoda Gosei Co Ltd | Engine head cover |
JPH06144223A (en) * | 1992-11-09 | 1994-05-24 | Railway Technical Res Inst | Structure for rolling stock |
JPH11354607A (en) * | 1998-06-10 | 1999-12-24 | Mitsubishi Chemical Corp | Hand for transfer apparatus |
JP4345188B2 (en) * | 2000-03-28 | 2009-10-14 | 宇部興産株式会社 | Flexible metal foil laminate and manufacturing method thereof |
ATE354466T1 (en) * | 2000-12-12 | 2007-03-15 | Core Technologies Inc C | LIGHTWEIGHT CIRCUIT BOARD WITH CORE CONTAINING CONDUCTOR MATERIAL |
-
2002
- 2002-12-02 CN CNB028294033A patent/CN100415505C/en not_active Expired - Fee Related
- 2002-12-02 KR KR1020057001568A patent/KR100989012B1/en not_active IP Right Cessation
- 2002-12-02 CA CA 2493963 patent/CA2493963C/en not_active Expired - Fee Related
- 2002-12-02 AU AU2002361894A patent/AU2002361894A1/en not_active Abandoned
- 2002-12-02 IL IL16593702A patent/IL165937A0/en unknown
- 2002-12-02 EP EP20020797524 patent/EP1525088B1/en not_active Expired - Lifetime
- 2002-12-02 US US10/519,029 patent/US7459215B2/en not_active Expired - Fee Related
- 2002-12-02 ES ES02797524T patent/ES2361827T3/en not_active Expired - Lifetime
- 2002-12-02 DE DE60239361T patent/DE60239361D1/en not_active Expired - Lifetime
- 2002-12-02 JP JP2004524463A patent/JP4474601B2/en not_active Expired - Fee Related
- 2002-12-02 WO PCT/US2002/041652 patent/WO2004011248A1/en active Application Filing
- 2002-12-02 TW TW91134930A patent/TW200401704A/en unknown
- 2002-12-02 AT AT02797524T patent/ATE500057T1/en active
-
2008
- 2008-10-28 US US12/259,816 patent/US7871705B2/en not_active Expired - Fee Related
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4759964A (en) * | 1983-10-10 | 1988-07-26 | Fischer Gesellschaft M.B.H. | Structural panel |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20090293663A1 (en) * | 2008-05-28 | 2009-12-03 | Advanced International Multitech Co., Ltd. | Robot arm |
CN102582146A (en) * | 2011-12-31 | 2012-07-18 | 杭州超探新材料科技有限公司 | Composite material with magnesium alloy as base body and manufacturing method thereof |
CN102582146B (en) * | 2011-12-31 | 2015-03-11 | 杭州超探新材料科技有限公司 | Composite material with magnesium alloy as base body and manufacturing method thereof |
US9884426B2 (en) | 2013-06-27 | 2018-02-06 | De-Sta-Co Europe Gmbh | Boom utilized in a geometric end effector system |
US9388278B2 (en) | 2013-10-04 | 2016-07-12 | Industrial Technology Research Institute | Release layer, substrate structure, and method for manufacturing flexible electronic device |
US20190134803A1 (en) * | 2015-08-10 | 2019-05-09 | Ozat 2000 (1999) Ltd. | Tools Made of Composite Material Structures Instead of Steel and Methods Thereof |
Also Published As
Publication number | Publication date |
---|---|
KR100989012B1 (en) | 2010-10-20 |
JP2005534587A (en) | 2005-11-17 |
CN100415505C (en) | 2008-09-03 |
US7871705B2 (en) | 2011-01-18 |
ES2361827T3 (en) | 2011-06-22 |
IL165937A0 (en) | 2006-01-15 |
EP1525088A1 (en) | 2005-04-27 |
CA2493963C (en) | 2011-07-05 |
US20060153669A1 (en) | 2006-07-13 |
CN1652924A (en) | 2005-08-10 |
ATE500057T1 (en) | 2011-03-15 |
DE60239361D1 (en) | 2011-04-14 |
US20090061242A1 (en) | 2009-03-05 |
EP1525088B1 (en) | 2011-03-02 |
TW200401704A (en) | 2004-02-01 |
WO2004011248A1 (en) | 2004-02-05 |
AU2002361894A1 (en) | 2004-02-16 |
JP4474601B2 (en) | 2010-06-09 |
KR20050059048A (en) | 2005-06-17 |
AU2002361894A8 (en) | 2004-02-16 |
CA2493963A1 (en) | 2004-02-05 |
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